DE60109521T2 - Vorrichtung zur lageregelung eines raumfahrzeuges - Google Patents

Vorrichtung zur lageregelung eines raumfahrzeuges Download PDF

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Publication number
DE60109521T2
DE60109521T2 DE60109521T DE60109521T DE60109521T2 DE 60109521 T2 DE60109521 T2 DE 60109521T2 DE 60109521 T DE60109521 T DE 60109521T DE 60109521 T DE60109521 T DE 60109521T DE 60109521 T2 DE60109521 T2 DE 60109521T2
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DE
Germany
Prior art keywords
spacecraft
axis
payload
reaction
bus
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60109521T
Other languages
German (de)
English (en)
Other versions
DE60109521D1 (de
Inventor
J. John ANAGNOST
C. Paul KIUNKE
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Raytheon Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Raytheon Co filed Critical Raytheon Co
Application granted granted Critical
Publication of DE60109521D1 publication Critical patent/DE60109521D1/de
Publication of DE60109521T2 publication Critical patent/DE60109521T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE60109521T 2000-02-01 2001-02-01 Vorrichtung zur lageregelung eines raumfahrzeuges Expired - Lifetime DE60109521T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US496140 2000-02-01
US09/496,140 US6463365B1 (en) 2000-02-01 2000-02-01 System and method for controlling the attitude of a space craft
PCT/US2001/003314 WO2001056882A1 (en) 2000-02-01 2001-02-01 System and method for controlling the attitude of a spacecraft

Publications (2)

Publication Number Publication Date
DE60109521D1 DE60109521D1 (de) 2005-04-28
DE60109521T2 true DE60109521T2 (de) 2006-02-16

Family

ID=23971402

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60109521T Expired - Lifetime DE60109521T2 (de) 2000-02-01 2001-02-01 Vorrichtung zur lageregelung eines raumfahrzeuges

Country Status (6)

Country Link
US (1) US6463365B1 (cg-RX-API-DMAC10.html)
EP (1) EP1165371B1 (cg-RX-API-DMAC10.html)
JP (1) JP4550347B2 (cg-RX-API-DMAC10.html)
DE (1) DE60109521T2 (cg-RX-API-DMAC10.html)
IL (1) IL145416A (cg-RX-API-DMAC10.html)
WO (1) WO2001056882A1 (cg-RX-API-DMAC10.html)

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* Cited by examiner, † Cited by third party
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GB0203950D0 (en) * 2002-02-20 2002-04-03 Astrium Ltd Method and system for balancing thrust demands
US6648274B1 (en) * 2002-04-12 2003-11-18 David A. Bailey Virtual reaction wheel array
US7216036B2 (en) * 2002-07-16 2007-05-08 The Charles Stark Draper Laboratory, Inc. Integrated inertial stellar attitude sensor
US6990396B2 (en) * 2002-12-13 2006-01-24 The Boeing Company Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector
US7025307B2 (en) * 2002-12-13 2006-04-11 The Boeing Company Method and apparatus for solar tacking momentum maintenance in long-duration deployment of a large reflector
US7437222B2 (en) * 2005-07-28 2008-10-14 The Boeing Company Gimbal disturbance calibration and compenstion
DE602006012795D1 (de) * 2006-01-19 2010-04-22 Thales Sa Vorrichtung zur Regelung der relativen Positionen von einer Gruppe in Formation fliegender Raumschiffe durch Analyse von Zweifrequenzsignalen
US8019493B1 (en) * 2007-07-20 2011-09-13 Lockheed Martin Corporation Spacecraft thruster torque feedforward calibration system
KR101008176B1 (ko) * 2008-12-30 2011-01-13 한국항공우주연구원 반작용휠과 추력기 기반 자세제어기를 동시에 이용한 자세기동 및 가제어성 향상 방법
WO2011100482A2 (en) * 2010-02-10 2011-08-18 Scott Gregory Dietz Motorized apparatus and moment imparting device
US10192173B2 (en) 2010-07-02 2019-01-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration System and method for training of state-classifiers
US8640994B1 (en) * 2010-09-27 2014-02-04 The Boeing Company Agile dedicated spacecraft for spinning microwave imagers and sounders
US9764858B2 (en) * 2015-01-07 2017-09-19 Mitsubishi Electric Research Laboratories, Inc. Model predictive control of spacecraft
RU2594057C1 (ru) * 2015-02-02 2016-08-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ одноосной ориентации космического аппарата вытянутой формы
RU2594054C1 (ru) * 2015-02-02 2016-08-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ одноосной ориентации космического аппарата вытянутой формы
RU2594056C1 (ru) * 2015-02-02 2016-08-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ одноосной ориентации космического аппарата вытянутой формы
CN106484929B (zh) * 2015-08-26 2019-06-28 上海宇航系统工程研究所 一种月球探测航天器多状态转动惯量计算方法
CN105843244A (zh) * 2016-06-02 2016-08-10 北京航空航天大学 一种基于输出反馈的挠性航天器精细姿态控制方法
JP2020062951A (ja) * 2018-10-17 2020-04-23 富士通株式会社 飛翔機
US11279501B2 (en) * 2018-10-25 2022-03-22 General Atomics Satellite attitude control system using eigen vector, non-linear dynamic inversion, and feedforward control
US12172660B2 (en) 2021-03-03 2024-12-24 United States Of America As Represented By The Administrator Of Nasa Method and system for collaborative task-based allocation between human and autonomous systems
US12649590B1 (en) 2023-10-06 2026-06-09 Eagle Technology, Llc Outer space-based vehicle with a payload steering arrangement

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0134288B1 (de) * 1983-09-03 1988-05-11 ERNO Raumfahrttechnik Gesellschaft mit beschränkter Haftung Variabel konfigurierbares Satellitensystem
US4723735A (en) * 1984-12-28 1988-02-09 The Charles Stark Draper Laboratory, Inc. Energy storage attitude control and reference system
US4824052A (en) * 1987-06-18 1989-04-25 Hughes Aircraft Company Nutation sensor and nutation control system for a dual-spin stabilized satellite
US5067673A (en) 1990-02-07 1991-11-26 Hughes Aircraft Company Essentially passive method for inverting the orientation of a dual spin spacecraft
US5131611A (en) * 1991-04-26 1992-07-21 The Perkin-Elmer Corporation Method and apparatus for reactionless rotation
US5441222A (en) * 1993-04-26 1995-08-15 Hughes Aircraft Company Attitude control of spinning spacecraft
US5667171A (en) * 1995-04-28 1997-09-16 Hughes Aircraft Company Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device
US5751078A (en) * 1996-10-03 1998-05-12 Lockheed Martin Corp. Missiles & Space Reactionless, momentum compensated payload positioner
US6068218A (en) * 1997-05-14 2000-05-30 Hughes Electronics Corporation Agile, spinning spacecraft with sun-steerable solar cell array and method
US6152402A (en) * 1999-04-07 2000-11-28 Hughes Electronics Corporation Dual spin zero momentum satellite system

Also Published As

Publication number Publication date
IL145416A (en) 2005-03-20
WO2001056882A1 (en) 2001-08-09
JP4550347B2 (ja) 2010-09-22
EP1165371A1 (en) 2002-01-02
DE60109521D1 (de) 2005-04-28
JP2003521424A (ja) 2003-07-15
IL145416A0 (en) 2002-06-30
EP1165371B1 (en) 2005-03-23
US6463365B1 (en) 2002-10-08

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